An approximate analytical method for calculating the trajectories of a flight vehicle in the atmosphere

Details An approximate analytical method for calculating the trajectories of a flight vehicle in the atmosphere An approximate analytical method for calculating the trajectories of a flight vehicle in the atmosphere

Apr 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983primm..47..348i&link_type=abstract

Prikladnaia Matematika i Mekhanika (ISSN 0032-8235), vol. 47, Mar.-Apr. 1983, p. 348-352. In Russian.

Physics

Atmospheric Entry, Flight Vehicles, Planetary Atmospheres, Spacecraft Trajectories, Trajectory Analysis, Approximation, High Speed, Planetary Rotation, Trajectory Optimization

Scientific paper

An approximate method is proposed for calculating the trajectories of a flight vehicle in the atmosphere with allowance for the ablation of the vehicle and the rotation of the planet. It is shown that the method can be effectively used for calculating the entry of a flight vehicle into the dense layers of the atmosphere at high velocities. Numerical examples are presented.

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